Attitude control problem for rigid spacecraft with highly nonlinear characteristics has attracted a great deal of interest for its important application [130],[196]. The attitude motion of a rigid body is represented by a set of two vector equations, namely, the kinematic equation which relates to the time derivatives of the orientation angles to the angular velocity vector and the dynamic equation which describes the time evolution of the angular velocity vector [262]. In [247], passivity-based control is proposed to ensure the asymptotical convergence of the attitude tracking without angular velocity measurements.
Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances
Lect.Notes Control
2013-01-01
27 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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